SECTION 7 CESSNA
AIRPLANE AND SYSTEM DESCRIPTION MODEL T182T NAV III
GFC 700 AFCS
U.S.
INSTRUMENT PANEL
The instrument panel (Refer to Figure 7-2) is of all metal construction
and is installed in sections so equipment can be easily removed for
maintenance. The glareshield, above and projecting aft from the
instrument panel, limits undesirable reflections on the windshield from
lighted equipment and displays mounted in the instrument panel.
The Nav III instrument panel contains the Garmin Display Unit (GDU)
Primary Flight Display (PFD) and Multifunction Display (MFD) and the
Garmin Audio Panel. For specific details regarding the instruments,
switches, circuit breakers and controls on the instrument panel, refer to
the related topics in this section.
PILOT PANEL LAYOUT
The PFD, centered on the instrument panel in front of the pilot, shows
the primary flight instruments during normal operation. During engine
start, reversionary operation (MFD failure) or when the DISPLAY
BACKUP switch is selected, the Engine Indication System (EIS) is
shown on the PFD. Refer to the Garmin G1000 CRG for specific
operating information.
The Standby Battery (STBY BATT) switch is found at the upper left
corner of the pilot instrument panel on an internally lighted subpanel.
The switch positions (ARM/OFF/TEST) select the standby battery
operating modes. The rocker-type MASTER and AVIONICS switches
are found immediately below the standby battery switch.
The controls for adjusting instrument panel, equipment, and pedestal
lighting are found together on the subpanel below the MASTER and
AVIONICS switches. See the INTERNAL LIGHTING paragraphs of this
section for more information.
(Continued Next Page)
T182TPHBUS-00
7-10
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